JILIN-01 GAOFEN 3D 7, 52392 (Decayed)
Orbit data source: Space-Track
JILIN-01 GAOFEN 3D 7, 52392 was a payload satellite owned by Changguang WJ (CN) in LEO that was launched on Sat, 30 Apr 2022 UTC via a CHANG ZHENG 11 launch vehicle from the Yellow Sea Launch Area, China (YSLA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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52392 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Decayed Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
43 kg wet, 43 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 JILIN-01 GAOFEN 3D 7
1 52392U 22046E 26025.78508520 .10439097 25929-5 47896-3 0 9997
2 52392 97.4708 145.3613 0009170 275.8607 84.1648 16.42458800208631Epoch: 2026-01-25T18:50Z
TLE epoch observation values (Epoch: 2026-01-25T18:50:31.361Z)
Latitude
-0.00002°
Longitude
97.64042°
Altitude
161.918 km
Speed
7.809 km/s
True Right ascension
09h 41m 26s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:27:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.069 km
Perigee altitude
150.086 km
Semi-major axis
6,534.215 km
Eccentricity
0.00092
Inclination
97.4708°
RAAN
145.3613°
Arg. of periapsis
275.8607°
True anomaly
84.26935°
Mean anomaly
84.1648°
Eccentric anomaly
84.21707°
Mean motion
4.10916 °/min
Orbital period
87.61 mins
BSTAR
0.00047896
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Other satellites on launch #46 in the year 2022 (2022-04-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.JILIN-01 GAOFEN 3D 7 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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